As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION PER ALLEGIANT TASK 534107-01-1-001 A PROFILE WITH CORROSION AT FR59 WAS FOUND. DURING PROFILE REPLACEMENT ADDITIONAL HEAVY CORROSION WAS FOUND ON HOLES AR FR59 INNER FLANGE ANCHOR NUT AREAS RH SIDE BETWEEN STRG 38RH AND STRG 42RH, DUE TO THERE IS NOT DATA APPROVED TO REPAIR THE MENTIONED DAMAGE, DETAILS WERE SUBMMITED TO AIRBUS REQUESTING PERMANENT REPAIR INSTRUCTIONS UNDER AIRBUS DOSSIER 70558716 AND COOPESA EO COO-EO-2022-16540-R00 JOB A1M142 ITEM 1-58